N120J

Substantial
None

BUTLER SX-300 S/N: 60

Accident Details

Date
Saturday, June 12, 1999
NTSB Number
DEN99LA100
Location
HILL AFB, UT
Event ID
20001212X18978
Coordinates
41.119785, -111.979263
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A failure of the left main landing gear attachment for undetermined reasons.

Aircraft Information

Registration
Make
BUTLER
Serial Number
60
Engine Type
Reciprocating
Year Built
1988
Model / ICAO
SX-300 TL30
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
SX 300

Registered Owner (Current)

Name
RAINBOW SPORTS INC
Address
PO BOX 3370
City
ENID
State / Zip Code
OK 73702-3370
Country
United States

Analysis

On June 12, 1999, at 1200 mountain daylight time, a Butler SX-300 homebuilt experimental aircraft, N120J, sustained substantial damage when the left main landing gear collapsed during taxi from landing at Hill AFB, Ogden, Utah. The commercial pilot and sole occupant was not injured. Visual meteorological conditions prevailed for this air show flight operating under Title 14 CFR Part 91 and no flight plan was filed. The flight departed Salt Lake City, Utah, earlier in the day.

The pilot said he was taxiing the aircraft to the ramp following landing and the left main landing gear collapsed when he made a turn.

According to the Federal Aviation Administration (FAA) Inspector who examined the aircraft following the accident, the pilot had landing gear problems a few days before the accident. The pilot related to the FAA inspector that he had heard a loud "bang/thump" from the landing gear but could not find the origin.

In a post-accident examination, the FAA inspector examined the left landing gear and determined the strut's outer trunnion flange had cracked and broke free from its attachment bolt. The inspector said this action allowed the strut to rotate forward. With this rotation, the actuator ram threaded rod end bent, then snapped free from the self-aligning anti-friction rod end assembly. The strut continued forward and impacted the fuselage causing damage to a structural bulkhead. Both sides of the empennage sustained damage and exhibited wrinkled skin panels.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DEN99LA100